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Aviation and the Global Atmosphere

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<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

directly involved in ice formation is difficult to obtain from in situ measurements. On <strong>the</strong><br />

o<strong>the</strong>r h<strong>and</strong>, fresh soot particles do not act as efficient ice (deposition) nuclei in <strong>the</strong> exhaust<br />

(Rogers et al., 1998), consistent with <strong>the</strong> absence of contrails at temperatures above <strong>the</strong><br />

liquid water saturation threshold.<br />

Contrails observed near threshold formation conditions are thought to result from freezing of<br />

water on soot particles (Kärcher et al., 1996b; Schumann et al., 1996; Brown et al., 1997)<br />

(Figure 3-5). This result is supported by laboratory experiments (DeMott, 1990; Diehl <strong>and</strong><br />

Mitra, 1998) that provide evidence that soot may induce ice formation by heterogeneous<br />

immersion freezing at temperatures colder than about 250 K. Water activation of soot may<br />

result from <strong>the</strong> formation of at least a partial surface coating of H 2 SO 4 /H 2 O droplets, which<br />

likely develops for average to high fuel sulfur levels (Figure 3-5). Hence, more fuel sulfur<br />

leads to a greater number of ice particles. However, observations demonstrate that <strong>the</strong><br />

number of ice particles (diameter > 300 nm) in young contrails increases by only about 30%<br />

when <strong>the</strong> fuel content increases from 6 to 2700 ppm (Petzold et al., 1997), as model<br />

simulations of contrail formation also show (Kärcher et al., 1998a).<br />

Contrails at threshold conditions appear to be formed for very low (2 ppm) fuel sulfur content<br />

in <strong>the</strong> same manner as for average fuel sulfur content (260 ppm) (Busen <strong>and</strong> Schumann,<br />

1995), but <strong>the</strong>ir properties differ measurably for larger fuel sulfur content (Schumann et al.,<br />

1996). This result suggests that soot may take up water even at zero fuel sulfur content,<br />

though this uptake may be enhanced in <strong>the</strong> presence of sulfur emissions (Kärcher et al.,<br />

1998a; see Figure 3-5).<br />

Figure 3-5: Soot activation <strong>and</strong> heterogeneous freezing in young<br />

The presence of liquid coatings may alter <strong>the</strong> chemical reactivity of dry exhaust soot, which aircraft exhaust plumes (Kärcher, 1998a).<br />

is poorly known (Chapter 2). Soot particles acting as freezing nuclei have <strong>the</strong> potential to<br />

alter cirrus cloud properties (see Section 3.4). Present observations do not rule out <strong>the</strong><br />

possibility that aircraft soot particles can act as freezing nuclei in cirrus formation, perhaps even without a H2SO4 /H2O coating. Information is lacking on how <strong>the</strong><br />

chemical reactivity <strong>and</strong> freezing properties of soot might change in aging plumes from interactions with background gases <strong>and</strong> particles or as a result of aerosol<br />

processing in contrails.<br />

Table 3-2: Emission indices <strong>and</strong> estimated global emission rates of exhaust products of <strong>the</strong> present (1992) aircraft fleet using representative emission<br />

indices. Emission sources o<strong>the</strong>r than aircraft <strong>and</strong> estimated magnitudes of <strong>the</strong>se emissions are listed in <strong>the</strong> last two columns. Values in paren<strong>the</strong>ses indicate<br />

estimated range (adapted from Fabian <strong>and</strong> Kärcher, 1997; Schumann, 1994).<br />

http://www.ipcc.ch/ipccreports/sres/aviation/035.htm (5 von 6)08.05.2008 02:41:58

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